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GB212010A - Reversible turbine engine - Google Patents

Reversible turbine engine

Info

Publication number
GB212010A
GB212010A GB3502422A GB3502422A GB212010A GB 212010 A GB212010 A GB 212010A GB 3502422 A GB3502422 A GB 3502422A GB 3502422 A GB3502422 A GB 3502422A GB 212010 A GB212010 A GB 212010A
Authority
GB
United Kingdom
Prior art keywords
offsets
blades
reversible turbine
turbine engine
reversible
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB3502422A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB3502422A priority Critical patent/GB212010A/en
Publication of GB212010A publication Critical patent/GB212010A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/30—Non-positive-displacement machines or engines, e.g. steam turbines characterised by having a single rotor operable in either direction of rotation, e.g. by reversing of blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

212,010. Yorston, J. K., and Ford, C. H. Dec. 22, 1922. Reversing. - In a reversible turbine of the kind comprising rotor and stator blades which are formed in one part C of their length for forward driving and in the other part D for reverse driving the blades are offset laterally at E between the two portions C, D, the offsets overlapping to form a continuous ring as shown in Fig. 3. Check rings F may be sweated to the offsets or may be constituted by the offsets themselves, these having extensions which are ground to the correct dimensions. When blades of this type are used in multistage turbines they are fitted to the high and intermediate pressure stages only, and means are provided for educting the exhaust from the intermediate stage so that the low pressure section revolves idly.
GB3502422A 1922-12-22 1922-12-22 Reversible turbine engine Expired GB212010A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3502422A GB212010A (en) 1922-12-22 1922-12-22 Reversible turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3502422A GB212010A (en) 1922-12-22 1922-12-22 Reversible turbine engine

Publications (1)

Publication Number Publication Date
GB212010A true GB212010A (en) 1924-03-06

Family

ID=10372889

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3502422A Expired GB212010A (en) 1922-12-22 1922-12-22 Reversible turbine engine

Country Status (1)

Country Link
GB (1) GB212010A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105715305A (en) * 2016-04-19 2016-06-29 中国船舶重工集团公司第七�三研究所 Backing turbo double-channel one-drive-two movable blade structure for gas turbine
CN109505664A (en) * 2019-01-25 2019-03-22 中国船舶重工集团公司第七0三研究所 A kind of marine gas turbine with the double-deck adjustable guide vane can reverse power turbine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105715305A (en) * 2016-04-19 2016-06-29 中国船舶重工集团公司第七�三研究所 Backing turbo double-channel one-drive-two movable blade structure for gas turbine
CN105715305B (en) * 2016-04-19 2017-12-08 中国船舶重工集团公司第七�三研究所 It is a kind of for gas turbine can the movable vane structure of one band of backing turbine binary channels two
CN109505664A (en) * 2019-01-25 2019-03-22 中国船舶重工集团公司第七0三研究所 A kind of marine gas turbine with the double-deck adjustable guide vane can reverse power turbine
CN109505664B (en) * 2019-01-25 2023-09-08 中国船舶重工集团公司第七0三研究所 Marine gas turbine power turbine that can reverse with double-deck rotatable stator

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